2. Layover Inspection Schedule Issue 06

7/25/2019 2. Layover Inspection Schedule Issue 06

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LAYOVER INSPECTION SCHEDULE

(AIRBUS A320 AIRCRAFT WITH V2527-A5 ENGINES)

APPROVAL IGO/E&M/Approval/Insp.Sch/22 dated: 15.06.2015 EFFECTIVITY:IGO ALL

INTERVAL To be performed once every 36 calendar hoursISSUE: 06 Dated: 15.06.2015

PAGE:1 of 17

FORM NO.IGO/E&M/A320/LO/41A

A/C REG. ______________ DATE: ______________ STATION: ________________

WORK ORDER NO.______________ STAMP (PLANNING DEPT.) _____________

CHECKED BY:

DIVISION NAME DATE SIGNATURE

TECH RECORDS


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INSTRUCTIONS TO THE CERTIFYING STAFF

1.

ENSURE THAT YOU HAVE REQUIRED TOOLS, EQUIPMENT, SPARES AND TECHNICAL LITERATURE PRIOR TO COMMENCEMENT OF

MAINTENANCE TASK.

2. ALL WARNINGS, CAUTIONS DETAILED IN THE REFERENCE TECHNICAL LITERATURE SHALL BE ADHERED TO WHILE PERFORMING

THE RESPECTIVE MAINTENANCE TASK.

3. CARRY OUT FUNCTIONAL TEST OF ALL SYSTEMS THAT WERE DISTURBED DURING THE COURSE OF INSPECTION AND MAINTAIN

RECORDS.

4. RAISE A MAINTENANCE WORK ORDER FOR ANY ABNORMAL FINDINGS OBSERVED WHILE PERFORMING THE INSPECTION

SCHEDULE.

5. WHENEVER AN AREA IS OPENED, INSPECT THE ADJACENT STRUCTURE/COMPONENT ALSO, AND RECORD ABNORMALITY IF

NOTICED, IN A SEPARATE MAINTENANCE WORK ORDER.

6. INSPECTION DATA SHOULD BE RECORDED BY CERTIFYING STAFF AS PER TASK CARD/ WORK ORDER DETAILS (IF APPLICABLE).

7. WHENEVER VALUES ARE TO BE CHECKED THE SAME ARE TO BE RECORDED AGAINST THE CORRESPONDING INSPECTION ITEM.

8. CERTIFY EACH MAINTENANCE STEP IN THE SCHEDULE/WORK ORDER AFTER ITS COMPLETION WITH TIME AND DATE.

9.

WHILE CARRYING OUT THE INSPECTION IN OPEN AIR ENSURE THE WEATHER AND ENVIRONMENT IS CONDUCIVE TO CARRYOUT THE INSPECTION PROPERLY.

10.ALWAYS USE CALIBRATED MEASURING INSTRUMENTS/EQUIPMENTS.

11.ENSURE THAT THE COMPONENT HAS APPROPRIATE SERVICEABLE TAG BEFORE INSTALLING ON THE AIRCRAFT.

12.REVIEW THE AIRCRAFT TECH LOG / CABIN DEFECT LOG FOR ANY PILOT / CABIN CREW DEFECT REPORTS. TAKE APPROPRIATE

RECTIFICATION ACTIONS.

13.REFER ADD/CDD PAGES OF TECH LOG FOR ANY DEFFERED DEFECT AND TAKE APPROPRIATE ACTION.

14.THE TERM INSPECTION/CHECK WHEREVER USED IN THIS SCHEDULE MEANS THAT THE ITEM HAS TO BE CHECKED FOR

SECURITY, CLEANLINESS, CORROSION, DETERIORATION, WEAR, CRACKS, DENTS, SCORES, CUTS, DISTORTION VISUAL EVIDENCE

OF BOWING, OVERHEATING, FREEDOM FROM OBSTRUCTION, LEAKS, LOCKING AND ANY OTHER DAMAGE.

15.THE CMR TASKS ARE MARKED AS (CMR).

16.THE ALS TASKS ARE MARKED AS (ALI).

17.THE CERTIFYING STAFF SIGNING THE CRS SHOULD ENSURE THAT ALL THE TASKS IN THE SCHEDULE ARE SIGNED OFF AND

SHOULD SIGN AND STAMP ON THE COLUMN PROVIDED AT THE BOTTOM OF EACH PAGE OF THE SCHEDULE.

DEFINITIONS:1. AIRWORTHINESS LIMITATION SECTION (ALS): ALS IS THE REPOSITORY FOR STAND-ALONE DOCUMENTS THAT CONSTITUTES

INSTRUCTIONS FOR CONTINUOUS AIRWORTHINESS. THE TASKS FROM ALS ARE INCLUDED IN THE MAINTENANCE PROGRAM AS

AIRWORTHINESS LIMITATION ITEM (ALI). IT COMPRISES OF DAMAGE TOLERANT AIRWORTHINESS LIMITATION ITEMS (DT ALI),

CERTIFICATION MAINTENANCE REQUIREMENTS (CMR) TASK ARISING FROM SYSTEM SAFETY ASSESSMENT WHICH ARE

ASSOCIATED WITH MOST SIGNIFICANT FAILURE CONDITIONS, AGEING SYSTEMS MAINTENANCE (ASM) & FUEL AIRWORTHINESS

LIMITATIONS (FAL).

2. EXTENDED DIVERSION TIME OPERATIONS (EDTO): THE EXTENDED DIVERSION TIME OPERATIONS (EDTO) IS AN OPERATION BY

AN AIRPLANE WITH TWO OR MORE TURBINE ENGINES WHERE THE DIVERSION TIME TO AN EN-ROUTE ALTERNATE

AERODROME IS GREATER THAN 60 MINUTES.

3. ELECTRICAL WIRING INTERCONNECTION SYSTEM (EWIS): EWIS RELATED TASKS COMPRISE OF THE ATA 20 TASKS, THE

LIGHTNING / HIGH INTENSITY RADIATED FIELDS (L/HIRF) TASKS AND ALL ZONAL INSPECTIONS IDENTIFIED EXCEPT THOSE

ASSOCIATED WITH MAJOR EXTERNAL ZONES (100, 200, 300 ETC). THESE TASKS ARE IDENTIFIED BY (EWIS) IN PARENTHESIS

FOLLOWING THE TASK DESCRIPTION.4. DETAILED INSPECTION (DI): AN INTENSIVE EXAMINATION OF A SPECIFIC ITEM, INSTALLATION OR ASSEMBLY TO DETECT

DAMAGE, FAILURE OR IRREGULARITY. AVAILABLE LIGHTING IS NORMALLY SUPPLEMENTED WITH A DIRECT SOURCE OF GOOD

LIGHTING AT AN INTENSITY DEEMED APPROPRIATE. INSPECTION AIDS SUCH AS MIRRORS, MAGNIFYING LENSES ETC MAY BE

NECESSARY. SURFACE CLEANING AND ELABORATE ACCESS PROCEDURES MAY BE REQUIRED.

5. GENERAL VISUAL INSPECTION (GVI): A VISUAL EXAMINATION OF AN INTERIOR OR EXTERIOR AREA, INSTALLATION OR

ASSEMBLY TO DETECT OBVIOUS DAMAGE, FAILURE OR IRREGULARITY. THIS LEVEL OF INSPECTION IS MADE FROM WITHIN

TOUCHING DISTANCE UNLESS OTHERWISE SPECIFIED. A MIRROR MAY BE NECESSARY TO ENSURE VISUAL ACCESS TO ALL

SURFACES IN THE INSPECTION AREA. THIS LEVEL OF INSPECTION IS MADE UNDER NORMALLY AVAILABLE LIGHTING

CONDITIONS SUCH AS DAYLIGHT, FLASHLIGHT OR DROP-LIGHT AND MAY REQUIRE REMOVAL OR OPENING OF ACCESS PANELS

OR DOORS. STANDS, LADDERS OR PLATFORMS MAY BE REQUIRED TO GAIN PROXIMITY TO THE AREA BEING CHECKED.

6. VISUAL CHECK (VC): AN OBSERVATION TO DETERMINE THAT AN ITEM IS FULFILLING ITS INTENDED PURPOSE. DOES NOT

REQUIRE QUANTITATIVE TOLERANCES. THIS IS A FAILURE FINDING TASK.

7. OPERATIONAL CHECK (OP):A TASK TO DETERMINE THAT AN ITEM IS FULFILLING ITS INTENDED PURPOSE. DO NOT REQUIRE

QUANTITATIVE TOLERANCES. THIS IS A FAILURE FINDING TASK.

8. FUNCTIONAL TEST (FU):A QUANTITATIVE CHECK TO DETERMINE IF ONE OR MORE FUNCTIONS OF A SYSTEM/SUB-SYSTEM OR

COMPONENT PERFORMS, WITHIN SPECIFIED LIMITS. THIS TASK MAY CALL FOR THE USE OF SPECIAL TEST EQUIPMENT.


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MANPOWER DETAILS

CERTIFYING STAFF

SN NAMELIC/APP./AUTH.

STAMPCAT SHORT SIGN.

SIGNATURE WITH

DATE

1

2

3

4

5

6

TECHNICIANS

SN NAME EMP. ID SHORT SIGN.SIGNATURE WITH

DATE

1

2

3

4

5

6

7

8


4/17




INTERVAL To be performed once every 36 calendar hoursISSUE: 06 Dated: 15.06.201 5

PAGE:4 of 17


A/C REG.: ______________ DATE: _______________ STATION: _______________

TOTAL NUMBER OF WORK ORDERS PERFORMED (SCHEDULED & UNSCHEDULED)

FLIGHT REPORT

DATE OF FLIGHT FLIGHT NO.

SECTOR FLOWN TIME IN AIRNO. OF

LDGS.

OIL UPLIFT (QTS.)

FROM TO AIRBORNE TOUCH DOWN IN AIR ENG 1 ENG 2 APU

TOTAL

PREVIOUS DAY RECORD CURRENT DAY RECORD TOTAL NOTE: THIS FLIGHT TIME LOG IS TO BE FILLED AND CERTIFIED BY THE APPROVED/AUTHORISED PERSON

A/C FLIGHT HRS.

A/C LANDINGS DATE TIMESIGN

(CERTIFYING STAFF)APP. / AUTH. STAMP CAT


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LIST OF REQUIRED TOOLS/EQUIPMENTS/CONSUMABLES

SN NOMENCLATUREPART NUMBER /

SPECIFICATIONQTY

1. Warning Notices Not Specific As Required

2. Suitable Access Platforms Not Specific As Required

3. Tyre Pressure Gauge Not Specific 01

4.Low Pressure Dry Nitrogen Gas source and

Charging Equipment.Not Specific 01

5. Ground Safety lock of NLG Downlock D23080000 01

6. Ground Lock Sleeve of MLG Downlock 460007280 02

7. Engine Oil MIL PRF 23699 As Required

8. Hydraulic Fluid

Skydrol LD4

CML Ref : 02-003D or

02-506

As Required

9. Mineral Hydraulic Fluid MIL PRF 5606H As Required

10.

Fuel Tank Draining Kit

a)

Adapting Pipe Water draining from fuel

tank.

b) PurgerWater drain for wing tanks.

c) Water Drain purger for centre tank.

98A28101000000

or

98D28104000000

98A28104000000

98A28104000002

01

01

01

01

11. One liter Glass Jar for fuel sample Not Specific 01

12. Fuel drain Container (metallic) 10 liters 01

13. Fuel sampling kit.Aquadis Detector

(HYDROKIT)As Required

14. Pin-Safety (Towing Pin) D23156000 1

15. Cover-Total Temperature Sensor 98A10001013000 2

16. Cover-Pitot Probe 98A10001005000 3

17. Cover-Slip On Angle Of Attack Sensor 98A10001500000 3

18. Cover-Static Probe98D10103500042

98D101035000434


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SIGNATURE

(CERTIFYING STAFF)AUTH. STAMP

FORM NO.IGO/E&M/A320/LO/41ARE

THIS SCHEDULE CONSISTS 33 TASKS

SN DESCRIPTIONSKILL

CODETECH

CERTIFYING

STAFF

ARRIVAL

1 Install the wheel chocks.

REF: AMM TASK 10-11-00-555-015AF

2 Install the nose landing gear and the main landing gear ground lock safety

devices (as necessary). REF: AMM TASK 32-00-00-481-001AF

3If aircraft towing is required, place the towing lever in the "towing position"

and install pin.

REF: AMM TASK 09-10-00-860-092

AF

4 Install Pitot, Static covers and other blanks.

REF: AMM TASK 10-11-00-555-069

AF

5Review the aircraft technical log and start corrective actions as necessary.

AF

NOTE: If the aircraft electrical network is not energized, perform items 6 and

7 otherwise continue with item 8

AF

6 Do a safety check of the flight compartment for proper position of thecontrols.

AF

7 Energize the aircraft electrical network.

REF: AMM TASK 24-41-00-861-002

AF

8 ENGINE OIL

(MPD 791000-I1-1-IGO) REF: AMM TASK 12-13-79-610-011

Check oil level and replenish.

WARNING: IF NECESSARY TO REMOVE THE OIL TANK CAP, YOU MUST

WAIT A MINIMUM OF 5 MINUTES AFTER ENGINE SHUT-

DOWN TO ALLOW PRESSURE IN OIL TANK TO DECREASE.

WARNING: OIL IS DANGEROUS IF IT IS ALLOWED TO BE ABSORBEDTHROUGH THE SKIN AND INTO THE BODY. IMMEDIATELY

FLUSH THE OIL WITH WATER.

CAUTION: DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE

ENGINE BACK TO THE OIL TANK.

CAUTION: IF THE ENGINE WAS STOPPED FOR MORE THAN ONE HOUR,

DO SPECIFIC MAINTENANCE ACTION (REFER SUBTASK 12-13-

79-869-051) TO MAKE SURE THAT OIL LEVEL IS CORRECT. THIS

WILL PREVENT OVERSERVICING IF OIL IS ADDED.

i. For NON-EDTO A/C:

Do a check of engine oil level as per AMM 12-13-79-610-011

and replenish, if required. Record the uplift in the aircraft

technical log.

EN


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SIGNATURE



SN DESCRIPTIONSKILLCODE

TECHCERTIFYING

STAFF

ii. For EDTO certified A/C:

a)

Do a check of the engine oil level on the tank sight gauge

within a period of 5 to 60 minutes after engine shutdown.

If the oil tank sight glass shows less than FULL, replenish

the oil tank to FULLlevel. Compute oil consumption since

last uplift and record in the aircraft technical log.

b) Check no oil filter CLOG indication on ECAM ENG Page.

Record Oil uplift:

Engine No. 1 ........... Qts Engine No. 2 ...Qts

Also record the oil uplift in Tech Log and on page no.4 of this schedule.

EN

9 APU OIL

REF: AMM TASK 12-13-49-612-001

CAUTION: IF POSSIBLE, WAIT AT LEAST 1 HOUR AFTER THE APU SHUT

DOWN TO ALLOW THE OIL TO BECOME COOL BEFORE YOU

SERVICE THE SYSTEM. THIS WILL MAKE SURE THE SIGHT

GLASS READING IS ACCURATE.

i. For NON-EDTO A/C:

If ECAM APU page shows LOW OIL LEVEL message,

replenish APU oil tank to FULL level and record uplift in the

aircraft technical log.

ii. For EDTO certified A/C:a) If ECAM APU page shows LOW OIL LEVEL message,

replenish APU oil tank to FULL level. Compute oil

consumption since last uplift and record in the aircraft

technical log.

b) Check no Oil filter clog (APU Maintenance status on

ECAM.) Follow the TSM procedure if Class 2 message

indicates discrepancy with APU system including oil filter

clog.

Record Oil uplift.Qts.

Record following: APU S/N .. APU HRS .. APU CYC .Also record the oil uplift in Tech Log and on page no.4 of this schedule.

EN

10 HYDRAULIC RESERVOIR QUANTITY CHECK

WARNING: DO NOT GET HYDRAULIC FLUID ON THE SKIN OR EYES. FLUSH

WITH CLEAN WATER AND GET MEDICAL AID.

Do a fluid level check of the Green, Blue and Yellow hydraulic reservoirs

(On ECAM LOWER DISPLAY, HYD page).

Add hydraulic fluid to the reservoirs as necessary. Record uplift(s)

Green ..Qts. Blue Qts Yellow .. Qts

Also record the hydraulic uplift in Tech Log

AF


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SIGNATURE




TECHCERTIFYING

STAFF

EXTERNAL WALK AROUND (AIRFRAME)

11 INTEGRATED DRIVE GENERATOR

(MPD 242100-07-1) Ref. AMM 24-21-51-200-010

(NOTE: TO BE PERFORMED ON EDTO CERTIFIED AIRCRAFT ONLY).

CHECK IDG OIL LEVEL AND DIFFERENTIAL PRESSURE INDICATOR

Record Oil uplift:

IDG No. 1 ..... Qts IDG No. 2 ....Qts

Also record the oil uplift in Tech log.

EN

12 LOWER HALF OF FUSELAGE

(MPD ZL-100-01-1-IGO) REF: AMM TASK: 05-21-00-200-001

Do a general visual inspection of the lower half of the fuselage from ground as

far as visible, including:

Pitot probes, static ports and AOA sensors: No obstruction

(Inspection with protective covers removed)

Avionics equipment ventilation: Air inlet and air outlet valves

Batteries ventilation outlet (Venturi): No obstruction

Waste water drain mast Antennas: No damage

Wing and engine scan lights: Cleanliness

Wing-to-fuselage fairings and belly fairing

Anti-collision beacon light: Cleanliness

Radome: No damage, latches engaged and locked

Crew oxygen cylinder overpressure indicator: Green disc in place

(Near access door 812).

LP/HP GRD connection panelsCLOSED

Ram air inlet flap

Ram air intakes and outlets: No obstruction

Inspect the belly fairing access panels for missing fasteners.

Ensure that there are no signs of corrosion, cracks or damage.

AF

13 UPPER HALF OF THE FUSELAGE

(MPD ZL-200-01-1-IGO) REF: AMM TASK:05-22-00-200-001

Do a general visual inspection of upper half of fuselage from ground as far as

possible for signs of corrosion, cracks or damage, including:

Cockpit & cabin windows: adjoining structure

Emergency exits

Anti-collision beacon light: Cleanliness

Antennas: No damage


AF


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SIGNATURE




TECHCERTIFYING

STAFF

14 STABILIZERS AND CONE/REAR FUSELAGE


Do a general visual inspection of the rear fuselage with cone and stabilizers

from ground as far as visible, including:

THS and elevators: Damage, evidence of fluid leakage

Fin and rudder: Damage, evidence of fluid leakage

Static dischargers

Tail cone strobe light

Waste water drain mast

Outflow valve

Fuselage tail damage due to ground contact

Ensure that there is no sign of corrosion, cracks or damage.

AF

15 WING

(MPD ZL-500-01-1-IGO) REF: AMM TASK:05-25-00-200-001

WARNING: DO NOT EXTEND THE SLATS AND FLAPS WHEN THE THRUST

REVERSER COWLS ARE DEPLOYED IN THE 45 UNIT POSITION

Do a general inspection of LH and RH wings from ground as far as visible.

(A)RIGHT/LEFT WING LEADING EDGE

Do a general visual inspection of the wing leading edge from ground as far as

visible, including:

Slats

Leading edge access panels(pressure relief panels in place)

Surge tank NACA air intake: No obstruction

Surge tank overpressure protector: White cross visible


(B) RIGHT/LEFT WING TIP AND TRAILING EDGE

Do a general visual inspection of the wing tip and trailing edge from ground as

far as visible, including:

Navigation and strobe lights for condition

Static dischargers missing or damaged

Control surfaces, flaps and flap track fairings: Damage, evidence of

fluid leakage

Lower wing surface: Damage, evidence of fuel leakage

Wing tank overpressure protector: Burst disk in place (White cross

visible

Landing light: No damage, cleanliness


AF


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SIGNATURE




TECHCERTIFYING

STAFF

16 LANDING GEAR AND LANDING GEAR DOORS


Do a general visual inspection of the main and nose landing gears and landing

gear doors from ground as far as visible, including:

Doors and wheel well

Gear assembly structure: Damage, evidence of leakage

Shock absorber: Signs of leakage and normal extension

Shock absorber sliding tube: Scoring/damage, cleanliness,

(if necessary, make a clean cloth moist with mineral hydraulic fluid

(Mat. No. 02-001), clean tube and dry with a clean cloth)

Proximity detectors: Security, cleanliness

Brake units: Evidence of leakage or overheating


AF

17 DOORS


Do a general visual inspection of all pax, service and cargo doors from ground

for signs of corrosion, cracks or damage.

4 Passenger/Crew doors

3 cargo compartment doors

4 overwing emergency exits

Service panel doors, avionic compartment access doors,

AF

18 TANKS

(MPD 281100-01-2) REF: AMM TASK: 12-32-28-281-001

WARNING:

1.

OBEY THE FUEL SAFETY PROCEDURES. GROUND THE AIRCRAFT CORRECTLY.

2.

HEADSET SHOULD NOT BE WORN. CABLES/LINES CONNECTED TO THE

AIRCRAFT SHOULD NOT BE TOUCHED.

3.

FUELLING SHOULD NOT BE DONE DURING BAD WEATHER CONDITION.

4.

LIGHTENING IS DANGEROUS WHILE WORKING ON FUEL TANKS.

5.

ALWAYS CONNECT THE GROUND CABLE TO THE PARKING GROUND POINT

BEFORE CONNECTING TO THE AIRCRAFT. DO NOT ATTACH THE GROUNDCABLE TO AIRCRAFT FIRST AS THERE IS A RISK OF ELECTRIC SHOCK.

NOTE:

1.

IF POSSIBLE, DO THE WATER DRAIN PROCEDURE BEFORE A REFUEL.

ALTERNATIVELY, YOU MUST WAIT FOR ONE HOUR AFTER A REFUEL HAS

BEEN COMPLETED BEFORE YOU DO THE WATER DRAIN PROCEDURE.

2.USE THE GRAVITY PROCEDURE ONLY IF THERE IS MORE THAN 10%

CONTENT OF FUEL IN EACH TANK

3.

USE SUCTION PROCEDURE IF THERE IS LESS THAN 10% CONTENT OF FUEL

IN EACH TANK.

AF


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PAGE:11 of 17

SIGNATURE




TECHCERTIFYING

STAFF

Drain water from wing tanks and center tank at water drain valves

Take fuel samples from all tanks. Check for any contamination. Check water

contents in the samples with Aquadis detector (HYDROKIT).

After drainage, make sure that the drain valves are correctly closed and not

leaking.

AF

19 WHEELS

(MPD 324100-01-1) REF: AMM TASK: 32-41-00-210-003

Inspect Nose, RH / LH Main Landing Gear Wheels and Tyres for satisfactory

condition (Wear & Damage) including:

Wheels: Rim damage, sheared/missing tie bolts

Tyres: Wear, damage and signs of under inflation/over inflation.

NOTE: For tyre damage, cuts, chord breakage etc refer to AMM Task

32-41-00-210-002.

CAUTION:

1. TYRE PRESSURE MUST BE CHECKED WHEN THE TYRES ARE NOT HOT.

2. SERVICE TYRES WITH NITROGEN ONLY.

3. ON ANY DAY IF LOW TYRE PRESSURE IS SUSPECTED ON ANY WHEEL

DURING INSPECTION THEN CHECK THE TYRE PRESSURE OF THE

SUSPECTED WHEEL/S AND INFLATE TO MAXIMUM TYRE PRESSURE.

4. AT LINE STATION IF DRY NITROGEN GAS IS NOT AVAILABLE THEN AIR

MAY BE USED. BUT BEFORE USE IT MUST BE ENSURED THAT THE AIR

BEING USED HAS OXYGEN NOT MORE THAN 5% BY VOLUME.

HOWEVER IF AIR WITH UNKNOWN OXYGEN CONTENT IS USED THEN

THIS AIR SHOULD BE REMOVED FROM TYRES WITHIN 15 HOURS AND

THE TYRES CHARGED WITH DRY NITROGEN. ACCORDINGLY A

NOTING SHOULD BE REFLECTED IN DEFERRED MAINTENANCE AND

WORKORDER.

5. THE CHEMICAL REACTION BETWEEN THE OXYGEN IN THE TYRES AND

GASES FROM THE INNER LINER OF THE TYRE MAY CAUSE A TYRE

EXPLOSION.

Check and record tyre pressure and inflate to maximum specified tyre

pressure, if necessary

(TO BE DONE DURING NIGHT HALT ON SUNDAY, TUESDAY & THURSDAY)

NOTE: MLG Tyre Pressure - Min : 210 psi Max: 220 psi

NLG Tyre Pressure - Min : 178 psi Max: 187 psi

CAUTION: IN CASE TYRE PRESSURE IS FOUND BELOW 170 PSI FOR NLG OR

BELOW 190 PSI FOR MLG REFER AMM TASK 32-41-00-210-059 FOR FURTHER

ACTION.

AF


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SIGNATURE




TECHCERTIFYING

STAFF

INITIAL TYRE PRESSURE:

Main Wheels Nose Wheels

#1 #2 #3 #4 #1 #2

Tyre Pr.

(PSI)

FINAL TYRE PRESSURE:

Main Wheels Nose Wheels

#1 #2 #3 #4 #1 #2

Tyre Pr.

(PSI)

Record the following Data:

TP Gauge Serial No. ..

Gauge Calibration date: . Next due on

AF

20 MAIN LANDING GEAR BRAKES

(MPD 324227-01-1) REF: AMM TASK:32-42-27-210-003

WARNING: PUT SAFETY DEVICES AND WARNING NOTICES IN POSITION

BEFORE STARTING INSPECTION NEAR MLG AND THE RELATED

DOORS.

Functional check of brake heat pack for wear by use of the wear indicator

(parking brake applied)

Ensure that there are no leaks from brake assemblies and hydraulic lines.

AF

WASTE/WATER SERVICING

NOTE: In freezing conditions, drain the potable water system and the toilet

waste tank. Service before aircraft departure.

NOTE: Obey the cold weather maintenance procedure (Ref. TASK 12-31-38-

660-001).

NOTE: If the temperature in the aircraft is below 4 DEG.C (39.20 DEG.F) do

the pre-conditioning procedure (Ref. TASK 12-33-21-618-001).

AF

21 Ensure that the potable water system is serviced as required.

To fill the potable water system with electrical power (Ref. AMM TASK 12-15-

38-613-001).

To fill the potable water system without electrical power (Ref. AMM TASK 12-

15-38-613-002).

AF

22 Ensure that the toilet waste tank is serviced as required (Ref. AMM TASK 12-

16-38-613-001). AF


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SIGNATURE




TECHCERTIFYING

STAFF

FLIGHT COMPARTMENT

23 CREW OXYGEN SYSTEM

On the DOOR/OXY page (lower ECAM DU), ensure that the oxygen pressure is

indicated in Green

AF

24 AIRCRAFT DOCUMENTS

Check for the presence and validity (where applicable) of the followingdocuments. Torn/mutilated/missing/invalid documents must be replaced.

1.

Certificate of Registration

2.

Certificate of Airworthiness

3. Aircraft Station License

4.

Noise Certificate

5.

Permit to Operate

6.

Certificate of Insurance

7. Weight Schedule

8.

Airworthiness Review Certificate (ARC)

9.

Emergency Equipment Location Chart

10.

LOPA11.

MEL Vol 1 and Vol 2

12.

Flight Report Book (FRB)

13.

Dent & Buckle Chart

14.

Cabin Defect Log Book (CDLB)in passenger compartment.

AF

25 EMERGENCY EQUIPMENT:

Check the emergency equipment for presence, correct stowage & validity

(where applicable).

Refer Emergency Equipment Location Chart in Documents on-board file forlocation and quantity of the equipment.

1. Crash Axe

2.

Fire proof gloves

3.

Life vest for crew

4.

Portable fire extinguisher

5.

Portable Breathing Equipment

6. Flash light

7.

Escape Rope

AF


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SIGNATURE




TECHCERTIFYING

STAFF

PASSENGER COMPARTMENT

26 EMERGENCY EQUIPMENT

Check the emergency equipment for presence, correct stowage & validity

(where applicable).

Refer Emergency Equipment Location Chart in Documents on -board file for

location and quantity of the equipment.

1.

First Aid Kit

2.

Medical Kit3.

Universal Precaution Kit

4.

Megaphone

5. Life vest for cabin crew

6.

Life vest for infants

7.

Portable fire extinguisher

8.

Portable oxygen bottle & masks

9. Portable Breathing Equipment

10.

Manual Release Tools

11.

Portable ELT

12.

Flash lights

13. PAX Life Vests

14.

Automated External Defibrillators (AED)Ensure that the Green Ready light is blinking.

NOTE:

- If the Ready light is steady: The AED is in use or running a

self-test.

-

If the Ready light is off, the AED is chirping, and the i-

button is flashing: The following may be the probable

causes:

a)

A self-test error has occurred,

b)

there is a problem with the pads,

c)

the Infant/Child Key has been left installed,

d) the battery power is low.

Press the i-button for instructions.

-

If the Ready light is off but the AED is not chirping and the

i-button is not flashing: The following may be the probable

causes:

a)

there is no battery inserted,

b)

the battery is depleted,

c)

the defibrillator needs repair.

15. Additional Emergency Equipment on EDTO certified A/C:

a)

Survival Kit

b)

Over-wing Escape Life Lines

c) Supplemental Life Raft

d)

Portable ELT

AF


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SIGNATURE




TECHCERTIFYING

STAFF

27 DEMO KIT CONTENTS:

Check the FWD and AFT Demo Kits contentsas mentioned below:

SN Description FWD Demo Kit AFT Demo Kit

1 DEMO MASK 1 2

2 DEMO BELT 1 2

3 EXTENSION BELT 2 24 PAX INFO CARD 1 2

5 DEMO LIFE VEST 1 2

AF

28 General visual check of the left and right wing upper surface and control

surfaces, through cabin windows. AF

AIRCRAFT CLEANING

29 COCKPIT AREA

Check and clean the cockpit area including windshield & windows, crew and

observer seats, floor area and cockpit door.

AF

30 CABIN

Check passenger compartment for general cleanliness including PSU, Stowage

compartments in galleys, toilets, doors, ceiling and side wall panels.

Passenger seat upholstery, carpets and passenger windows.

AF

31 EXTERIOR CLEANING

REF: AMM TASK 12-21-11-615-002

External surface of fuselage, wing control surfaces, landing gear doors. Check

that fuselage exterior is free from streaks and deposits.

AF

EXTERNAL WALK AROUND (APU)

AUXILLARY POWER UNIT

32 Visual check of the APU area from ground for general condition:

Air intake

Doors: Closed and secured

Drain mast, drains and vents

Exhaust

Fire extinguisher overpressure discharge indicator: Red disc in place


EN


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PAGE:16 of 17

SIGNATURE




TECHCERTIFYING

STAFF

EXTERNAL WALK AROUND (ENGINES)

33 POWER PLANT, NACELLES AND PYLON

(MPD ZL-400-01-1-IGO) Ref: AMM Task: 05-24-00-200-001

Visual inspection of power plant, nacelles and pylon from ground as far as

visible(cowl doors closed) including:

Pylon fairing and fillets: No damage, pressure relief doors closed

Engine air inlet: lip and outer and inner skin, riveting, acoustic

panels, and visible probes and sensors (P2/T2)

Fan blades, annulus fillers and spinner: No damage

Fan rotor path, splitter fairing, inlet guide vanes, fan outlet guide

vanes and fan duct. Check Fan free rotation by hand.

External surface of the fan cowl doors and thrust reverser doors,

Doors closed and correctly latched. Access doors and pressure

relief doors in place, closed and secured.

Air inlets/outlets: No obstruction.

Translating sleeves correctly stowed.

CNA (Common Nozzle Assembly) and exhaust: Last stage LPT

blades, struts, nozzle and plug (for damage and metal deposit)

Drain mast and pylon drains: No obstruction, evidence of leakage.

Fan Exhaust: Acoustic lining, exit vanes, struts and thrust reverser

blocker doors.


EN


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PAGE:17 of 17

FORMNO IGO/E&M/A320/LO/41A

CERTIFICATE OF RELEASE TO SERVICE

ORGANIZATION NAME INTERGLOBE AVIATION LIMITED (INDIGO)

ORGANIZATION APPROVAL

REFERENCE

DAW, DELHI REGION LETTER NO. INDIGO/FAPP/1034 DATED 31/07/2006

CERTIFICATE OF RELEASE TO SERVICE IN ACCORDANCE WITH CAR 145

AIRCRAFT AIRBUS A320-232 MSN REGISTRATION TAH TAC

HAS BEEN MAINTAINED AS SPECIFIED IN THE WORK ORDERWORK ORDER

NO.

RECORD WORKORDER & TASKCARD NUMBERS (AS APPLICABLE), INCLUDING A BRIEF DESCRIPTION OF WORK

PERFORMED*

CERTIFIES THAT THE WORK SPECIFIED EXCEPT AS OTHERWISE SPECIFIED WAS CARRIED OUT IN ACCORDANCE WITH

CAR-145 AND IN RESPECT TO THAT WORK THE AIRCRAFT/AIRCRAFT COMPONENT IS CONSIDERED READY FOR

RELEASE TO SERVICE.

CERTIFYING

STAFF (NAME)SIGNATURE

LIC/APP./AUTH.

STAMP

LOCATION** DATE TIME

* REFERENCE TO APPROVED DATA USED TO PERFORM THE WORK

** LOCATION WHERE THE WORK WAS PERFORMED

FORM NO. IGO/E&M/CRS/No. 7 Issue 1

2. Layover Inspection Schedule Issue 06

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Transcript of 2. Layover Inspection Schedule Issue 06